View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67770U 26145.41297735 +.00000000 +00000-0 +38400-3 0 00004
2 67770 51.8972 221.3458 0000401 98.4318 261.6690 14.79919610 01
| Epoch (UTC): | 25 May 2026 09:54:41 |
| Eccentricity: | 0.0000401 |
| inclination: | 51.8972° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 221.3458° |
| argument of perigee: | 98.4318° |
| revolutions per day: | 14.79919610 |
| mean anomaly at epoch: | 261.6690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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